Rotor assembly with cooling air deflectors and method

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 5/08 (2006.01) F01D 11/00 (2006.01)

Patent

CA 2528668

A rotor assembly for a gas turbine engine, the rotor assembly comprises a plurality of cooling air deflectors mounted on the rotor assembly to redirect air to a manifold at a bottom side of a corresponding blade retention slot on the periphery of the rotor disk.

Un ensemble de rotor d'un moteur à turbines à gaz, l'ensemble de rotor comprend plusieurs déflecteurs d'air de refroidissement montés sur l'ensemble de rotor pour rediriger l'air vers un manifold à une paroi inférieure d'une fente de retenue de pale correspondante sur la périphérie du disque de rotor.

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